[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 20th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
235/08:52:24
380 -4
7 8
9 9
0
N/A -2
1 -1
3 230
7
000/00:34:48
761 7
4 -0
0 218
4
235/12:43:11
633 2
1 2
8 2
9
N/A 1
2 -0
6 230
9
000/00:06:23
265 -1
6 -0
1 219
8
Coasting Arc #1 (Orbit 2757)
---------------------------------------
Vector Time (GMT): 2012/230/15:17:36
814
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4583257
19 A = 6785516
75 meter
Y = -3380797
49 meter E =
0010909
Z = 3688335
31 I = 51
67376
XDOT = 5626
690058 Wp = 48
00633
YDOT = 2886
314036 meter/sec RA = 174
37893 deg
ZDOT = -4330
903195 TA = 88
13304
MA = 88
00810
Ha = 222
483 n
mi
Hp = 216
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15036933
04 X = 4602804
59
Y = -11091855
27 feet Y = -3329435
23 meter
Z = 12100837
62 Z = 3710647
71
XDOT = 18460
269220 XDOT = 5615
034641
YDOT = 9469
534240 feet/sec YDOT = 2949
169871 meter/sec
ZDOT = -14208
999983 ZDOT = -4303
597944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11581600
30 X = -3530071
77
Y = 14586271
83 feet Y = 4445895
65 meter
Z = 12193280
45 Z = 3716511
88
XDOT = -19302
059582 XDOT = -5883
267761
YDOT = -3500
322910 feet/sec YDOT = -1066
898423 meter/sec
ZDOT = -14096
432138 ZDOT = -4296
592516
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12230
67734617
00016717 00000-0 10270-3 0 9006
2 25544 51
6434 175
2832 0007199 330
1456 29
9284 15
53429035 27584
Satellite: ISS
Catalog Number: 25544
Epoch time: 12230
67734617 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 175
2832 deg
Eccentricity:
0007199
Arg of perigee: 330
1456 deg
Mean anomaly: 29
9284 deg
Mean motion: 15
53429035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2758
Checksum: 314
Coasting Arc #2 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2012/231/15:17:36
814
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5526830
65 A = 6788572
08 meter
Y = 3038233
56 meter E =
0009874
Z = -2496268
15 I = 51
71538
XDOT = -4302
624903 Wp = 4
67656
YDOT = -3466
118959 meter/sec RA = 169
40600 deg
ZDOT = 5318
610782 TA = 327
36360
MA = 327
42459
Ha = 222
538 n
mi
Hp = 216
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18132646
47 X = -5548267
93
Y = 9967957
87 feet Y = 2976309
11 meter
Z = -8189856
14 Z = -2523169
01
XDOT = -14116
223436 XDOT = -4289
382435
YDOT = -11371
781363 feet/sec YDOT = -3514
159273 meter/sec
ZDOT = 17449
510439 ZDOT = 5297
741526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14637384
24 X = 4461474
72
Y = -14562392
90 feet Y = -4438617
36 meter
Z = -8301234
34 Z = -2530216
23
XDOT = 15742
535555 XDOT = 4798
324837
YDOT = 5946
030355 feet/sec YDOT = 1812
350052 meter/sec
ZDOT = 17363
567179 ZDOT = 5292
415276
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12231
64230618
00016717 00000-0 10270-3 0 9017
2 25544 51
6444 170
4773 0007287 333
0515 27
0258 15
53454695 27739
Satellite: ISS
Catalog Number: 25544
Epoch time: 12231
64230618 = yrday
fracday
Element set: 901
Inclination: 51
6444 deg
RA of node: 170
4773 deg
Eccentricity:
0007287
Arg of perigee: 333
0515 deg
Mean anomaly: 27
0258 deg
Mean motion: 15
53454695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 300
Coasting Arc #3 (Orbit 2788)
---------------------------------------
Vector Time (GMT): 2012/232/15:17:36
814
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6177400
82 A = 6790829
72 meter
Y = -2601753
07 meter E =
0008655
Z = 1077814
50 I = 51
75230
XDOT = 2744
293290 Wp = 96
00388
YDOT = 4058
033002 meter/sec RA = 164
44244 deg
ZDOT = -5893
135191 TA = 72
33332
MA = 72
23884
Ha = 222
734 n
mi
Hp = 216
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20267063
07 X = 6200799
33
Y = -8535935
28 feet Y = -2532542
64 meter
Z = 3536136
80 Z = 1107880
63
XDOT = 9003
586911 XDOT = 2727
338715
YDOT = 13313
756568 feet/sec YDOT = 4088
626239 meter/sec
ZDOT = -19334
433042 ZDOT = -5879
845143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16871317
26 X = -5142377
50
Y = 14074061
60 feet Y = 4289773
98 meter
Z = 3660566
06 Z = 1115740
54
XDOT = -11584
382282 XDOT = -3530
919720
YDOT = -8839
448590 feet/sec YDOT = -2694
263930 meter/sec
ZDOT = -19279
844787 ZDOT = -5876
496691
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12232
67158846
00016717 00000-0 10270-3 0 9024
2 25544 51
6443 165
3517 0007151 336
6384 23
4443 15
53430433 27897
Satellite: ISS
Catalog Number: 25544
Epoch time: 12232
67158846 = yrday
fracday
Element set: 902
Inclination: 51
6443 deg
RA of node: 165
3517 deg
Eccentricity:
0007151
Arg of perigee: 336
6384 deg
Mean anomaly: 23
4443 deg
Mean motion: 15
53430433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2789
Checksum: 305
Coasting Arc #4 (Orbit 2804)
---------------------------------------
Vector Time (GMT): 2012/233/15:17:36
814
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6443978
36 A = 6791140
63 meter
Y = 2069945
49 meter E =
0016838
Z = 406230
92 I = 51
78289
XDOT = -1106
527082 Wp = 25
25236
YDOT = -4639
448034 meter/sec RA = 159
48305 deg
ZDOT = 6010
852490 TA = 339
12102
MA = 339
18971
Ha = 222
826 n
mi
Hp = 216
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21141661
28 X = -6468619
35
Y = 6791159
73 feet Y = 1997747
16 meter
Z = 1332778
62 Z = 374866
66
XDOT = -3630
338197 XDOT = -1083
764693
YDOT = -15221
286202 feet/sec YDOT = -4651
694266 meter/sec
ZDOT = 19720
644652 ZDOT = 6005
532653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18024916
21 X = 5493994
46
Y = -12981568
99 feet Y = -3956782
23 meter
Z = 1203018
38 Z = 366680
00
XDOT = 7314
457522 XDOT = 2229
446653
YDOT = 12007
511150 feet/sec YDOT = 3659
889399 meter/sec
ZDOT = 19699
032913 ZDOT = 6004
265232
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12233
70085754
00016717 00000-0 10270-3 0 9037
2 25544 51
6444 160
2252 0007382 339
9678 20
1183 15
53488498 28054
Satellite: ISS
Catalog Number: 25544
Epoch time: 12233
70085754 = yrday
fracday
Element set: 903
Inclination: 51
6444 deg
RA of node: 160
2252 deg
Eccentricity:
0007382
Arg of perigee: 339
9678 deg
Mean anomaly: 20
1183 deg
Mean motion: 15
53488498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2805
Checksum: 315
Coasting Arc #5 (Orbit 2819)
---------------------------------------
Vector Time (GMT): 2012/234/15:17:36
814
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6373463
20 A = 6789808
82 meter
Y = -1391462
38 meter E =
0002666
Z = -1887664
69 I = 51
80591
XDOT = -539
016538 Wp = 60
17525
YDOT = 5164
764439 meter/sec RA = 154
52528 deg
ZDOT = -5631
717132 TA = 140
53675
MA = 140
51733
Ha = 222
922 n
mi
Hp = 216
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20910312
34 X = 6397718
94
Y = -4565165
30 feet Y = -1320054
83 meter
Z = -6193125
62 Z = -1856643
85
XDOT = -1768
426962 XDOT = -569
372456
YDOT = 16944
765220 feet/sec YDOT = 5158
566793 meter/sec
ZDOT = -18476
762245 ZDOT = -5634
409645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18330841
23 X = -5587240
41
Y = 11119119
66 feet Y = 3389107
67 meter
Z = -6064828
02 Z = -1848559
58
XDOT = -3124
348108 XDOT = -952
301303
YDOT = -15226
512825 feet/sec YDOT = -4641
041109 meter/sec
ZDOT = -18488
304022 ZDOT = -5635
235066
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12234
66578991
00016717 00000-0 10270-3 0 9044
2 25544 51
6440 155
4199 0007304 342
4301 17
6598 15
53464312 28209
Satellite: ISS
Catalog Number: 25544
Epoch time: 12234
66578991 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 155
4199 deg
Eccentricity:
0007304
Arg of perigee: 342
4301 deg
Mean anomaly: 17
6598 deg
Mean motion: 15
53464312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2820
Checksum: 307
Coasting Arc #6 (Orbit 2831)
---------------------------------------
Vector Time (GMT): 2012/235/09:09:48
761
Vector Time (MET): N/A
Weight (LBS) : 954598
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5506794
53 A = 6793315
08 meter
Y = -470016
83 meter E =
0015672
Z = 3933563
17 I = 51
80896
XDOT = 3376
960351 Wp = 22
04543
YDOT = -5554
279829 meter/sec RA = 150
83026 deg
ZDOT = 4072
815202 TA = 25
49657
MA = 25
41935
Ha = 230
728 n
mi
Hp = 218
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18066911
17 X = -5520237
73
Y = -1542049
97 feet Y = -531672
24 meter
Z = 12905390
98 Z = 3906778
85
XDOT = 11079
266243 XDOT = 3419
033708
YDOT = -18222
702852 feet/sec YDOT = -5516
281144 meter/sec
ZDOT = 13362
254600 ZDOT = 4089
322700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4057396
13 X = 1236694
34
Y = 17753095
35 feet Y = 5411143
46 meter
Z = 12794743
30 Z = 3899837
76
XDOT = -19410
688732 XDOT = -5916
377925
YDOT = -5222
246805 feet/sec YDOT = -1591
740826 meter/sec
ZDOT = 13430
923470 ZDOT = 4093
745474
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12235
43785161
00016717 00000-0 10270-3 0 9050
2 25544 51
6435 151
5725 0017151 342
3935 17
6619 15
50548775 28328
Satellite: ISS
Catalog Number: 25544
Epoch time: 12235
43785161 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 151
5725 deg
Eccentricity:
0017151
Arg of perigee: 342
3935 deg
Mean anomaly: 17
6619 deg
Mean motion: 15
50548775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2832
Checksum: 312
Coasting Arc #7 (Orbit 2833)
---------------------------------------
Vector Time (GMT): 2012/235/12:46:23
265
Vector Time (MET): N/A
Weight (LBS) : 954317
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5307133
55 A = 6800825
95 meter
Y = -4100404
95 meter E =
0010448
Z = 1149504
08 I = 51
83354
XDOT = 3735
304802 Wp = 47
00852
YDOT = 3176
383453 meter/sec RA = 150
05167 deg
ZDOT = -5874
225079 TA = 120
58360
MA = 120
48048
Ha = 230
901 n
mi
Hp = 219
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17411855
49 X = 5347006
67
Y = -13452772
15 feet Y = -4040834
29 meter
Z = 3771338
85 Z = 1175382
84
XDOT = 12254
937013 XDOT = 3728
043798
YDOT = 10421
205555 feet/sec YDOT = 3218
113133 meter/sec
ZDOT = -19272
391992 ZDOT = -5856
096941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20691809
05 X = -6306863
40
Y = 7428199
31 feet Y = 2264115
15 meter
Z = 3878618
31 Z = 1182202
86
XDOT = -8010
323029 XDOT = -2441
546459
YDOT = -12221
403091 feet/sec YDOT = -3725
083662 meter/sec
ZDOT = -19197
735596 ZDOT = -5851
469810
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12235
56677214
00016717 00000-0 10270-3 0 9064
2 25544 51
6444 150
9349 0014969 344
6809 15
3886 15
49977603 28349
Satellite: ISS
Catalog Number: 25544
Epoch time: 12235
56677214 = yrday
fracday
Element set: 906
Inclination: 51
6444 deg
RA of node: 150
9349 deg
Eccentricity:
0014969
Arg of perigee: 344
6809 deg
Mean anomaly: 15
3886 deg
Mean motion: 15
49977603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2834
Checksum: 347
Coasting Arc #8 (Orbit 2848)
---------------------------------------
Vector Time (GMT): 2012/236/12:46:23
265
Vector Time (MET): N/A
Weight (LBS) : 954317
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5127306
31 A = 6801045
76 meter
Y = 4367848
88 meter E =
0022827
Z = -828063
19 I = 51
86038
XDOT = -3649
706507 Wp = 8
62949
YDOT = -3162
217274 meter/sec RA = 145
11263 deg
ZDOT = 5961
918952 TA = 342
44545
MA = 342
52422
Ha = 231
034 n
mi
Hp = 219
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16821871
10 X = -5171744
89
Y = 14330212
86 feet Y = 4310263
66 meter
Z = -2716742
77 Z = -853079
38
XDOT = -11974
102714 XDOT = -3643
036283
YDOT = -10374
728590 feet/sec YDOT = -3202
993164 meter/sec
ZDOT = 19560
101548 ZDOT = 5944
205136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20259396
20 X = 6175063
96
Y = -8792764
77 feet Y = -2680034
70 meter
Z = -2820495
10 Z = -859686
91
XDOT = 7892
441208 XDOT = 2405
616080
YDOT = 11977
767652 feet/sec YDOT = 3650
823580 meter/sec
ZDOT = 19487
153571 ZDOT = 5939
684408
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12236
53387705
00016717 00000-0 10270-3 0 9076
2 25544 51
6446 146
1434 0015108 348
0540 12
0250 15
50002236 28497
Satellite: ISS
Catalog Number: 25544
Epoch time: 12236
53387705 = yrday
fracday
Element set: 907
Inclination: 51
6446 deg
RA of node: 146
1434 deg
Eccentricity:
0015108
Arg of perigee: 348
0540 deg
Mean anomaly: 12
0250 deg
Mean motion: 15
50002236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2849
Checksum: 277
Coasting Arc #9 (Orbit 2864)
---------------------------------------
Vector Time (GMT): 2012/237/12:46:23
265
Vector Time (MET): N/A
Weight (LBS) : 954317
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4969988
83 A = 6801258
29 meter
Y = -4624829
57 meter E =
0010210
Z = 470337
96 I = 51
88537
XDOT = 3533
630491 Wp = 50
09948
YDOT = 3178
134607 meter/sec RA = 140
17586 deg
ZDOT = -5995
959464 TA = 124
86089
MA = 124
76485
Ha = 231
177 n
mi
Hp = 219
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16305737
64 X = 5019050
46
Y = -15173325
35 feet Y = -4568977
74 meter
Z = 1543103
55 Z = 494601
01
XDOT = 11593
275889 XDOT = 3526
956209
YDOT = 10426
950811 feet/sec YDOT = 3217
612554 meter/sec
ZDOT = -19671
783020 ZDOT = -5978
809520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19848472
13 X = -6049814
30
Y = 10090797
13 feet Y = 3075674
97 meter
Z = 1643781
64 Z = 501024
64
XDOT = -7648
181693 XDOT = -2331
165780
YDOT = -11804
309117 feet/sec YDOT = -3597
953419 meter/sec
ZDOT = -19601
163507 ZDOT = -5974
434637
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12237
56544784
00016717 00000-0 10270-3 0 9083
2 25544 51
6446 141
0325 0014981 351
8064 8
2839 15
49993915 28650
Satellite: ISS
Catalog Number: 25544
Epoch time: 12237
56544784 = yrday
fracday
Element set: 908
Inclination: 51
6446 deg
RA of node: 141
0325 deg
Eccentricity:
0014981
Arg of perigee: 351
8064 deg
Mean anomaly: 8
2839 deg
Mean motion: 15
49993915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2865
Checksum: 337
Coasting Arc #10 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2012/238/12:46:23
265
Vector Time (MET): N/A
Weight (LBS) : 954317
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4741061
49 A = 6801254
63 meter
Y = 4852336
78 meter E =
0024536
Z = -136641
94 I = 51
90873
XDOT = -3467
517345 Wp = 16
63785
YDOT = -3226
150140 meter/sec RA = 135
24008 deg
ZDOT = 6037
323275 TA = 341
89596
MA = 341
98318
Ha = 231
310 n
mi
Hp = 218
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15554663
67 X = -4794305
18
Y = 15919740
09 feet Y = 4799021
58 meter
Z = -448300
32 Z = -159802
89
XDOT = -11376
369242 XDOT = -3460
511882
YDOT = -10584
482087 feet/sec YDOT = -3264
886981 meter/sec
ZDOT = 19807
491059 ZDOT = 6020
495337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19146525
94 X = 5835861
11
Y = -11344636
11 feet Y = -3457845
09 meter
Z = -544459
27 Z = -165951
19
XDOT = 7533
946234 XDOT = 2296
346812
YDOT = 11805
452325 feet/sec YDOT = 3598
301869 meter/sec
ZDOT = 19738
202336 ZDOT = 6016
204072
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12238
53253576
00016717 00000-0 10270-3 0 9098
2 25544 51
6451 136
2408 0015177 355
1078 4
9922 15
50034566 28807
Satellite: ISS
Catalog Number: 25544
Epoch time: 12238
53253576 = yrday
fracday
Element set: 909
Inclination: 51
6451 deg
RA of node: 136
2408 deg
Eccentricity:
0015177
Arg of perigee: 355
1078 deg
Mean anomaly: 4
9922 deg
Mean motion: 15
50034566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 309
Coasting Arc #11 (Orbit 2895)
---------------------------------------
Vector Time (GMT): 2012/239/12:46:23
265
Vector Time (MET): N/A
Weight (LBS) : 954317
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4538459
11 A = 6801286
25 meter
Y = -5066433
54 meter E =
0010167
Z = -234452
73 I = 51
92968
XDOT = 3381
235271 Wp = 49
74519
YDOT = 3299
644903 meter/sec RA = 130
30660 deg
ZDOT = -6017
096975 TA = 132
76271
MA = 132
67713
Ha = 231
425 n
mi
Hp = 218
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14889957
72 X = 4595914
62
Y = -16622157
28 feet Y = -5015360
41 meter
Z = -769201
87 Z = -212265
87
XDOT = 11093
291571 XDOT = 3373
315999
YDOT = 10825
606636 feet/sec YDOT = 3337
411763 meter/sec
ZDOT = -19741
131808 ZDOT = -6000
690489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18481319
98 X = -5633106
33
Y = 12513235
37 feet Y = 3814034
14 meter
Z = -677035
73 Z = -206360
49
XDOT = -7341
088118 XDOT = -2237
563658
YDOT = -11873
355973 feet/sec YDOT = -3618
998901 meter/sec
ZDOT = -19673
586702 ZDOT = -5996
509227
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12239
56408901
00016717 00000-0 10270-3 0 9108
2 25544 51
6452 131
1300 0015021 358
7638 1
3473 15
50013700 28968
Satellite: ISS
Catalog Number: 25544
Epoch time: 12239
56408901 = yrday
fracday
Element set: 910
Inclination: 51
6452 deg
RA of node: 131
1300 deg
Eccentricity:
0015021
Arg of perigee: 358
7638 deg
Mean anomaly: 1
3473 deg
Mean motion: 15
50013700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 270
Coasting Arc #12 (Orbit 2911)
---------------------------------------
Vector Time (GMT): 2012/240/12:46:23
265
Vector Time (MET): N/A
Weight (LBS) : 954317
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4271608
97 A = 6801046
20 meter
Y = 5239449
94 meter E =
0025713
Z = 574794
62 I = 51
94832
XDOT = -3352
706943 Wp = 24
67626
YDOT = -3400
539057 meter/sec RA = 125
37348 deg
ZDOT = 6007
580028 TA = 341
50015
MA = 341
59347
Ha = 231
554 n
mi
Hp = 218
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14014465
14 X = -4332672
29
Y = 17189796
38 feet Y = 5191340
73 meter
Z = 1885809
12 Z = 553895
34
XDOT = -10999
694695 XDOT = -3343
615221
YDOT = -11156
624202 feet/sec YDOT = -3437
980258 meter/sec
ZDOT = 19709
908227 ZDOT = 5991
315091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17545339
08 X = 5347819
35
Y = -13578494
26 feet Y = -4138725
05 meter
Z = 1798938
29 Z = 548316
39
XDOT = 7323
497454 XDOT = 2232
202024
YDOT = 12098
973354 feet/sec YDOT = 3687
767078 meter/sec
ZDOT = 19642
951925 ZDOT = 5987
171747
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12240
59563126
00016717 00000-0 10270-3 0 9115
2 25544 51
6454 126
0186 0015235 2
2705 357
8512 15
50067625 29125
Satellite: ISS
Catalog Number: 25544
Epoch time: 12240
59563126 = yrday
fracday
Element set: 911
Inclination: 51
6454 deg
RA of node: 126
0186 deg
Eccentricity:
0015235
Arg of perigee: 2
2705 deg
Mean anomaly: 357
8512 deg
Mean motion: 15
50067625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2912
Checksum: 284
Coasting Arc #13 (Orbit 2926)
---------------------------------------
Vector Time (GMT): 2012/241/12:46:23
265
Vector Time (MET): N/A
Weight (LBS) : 954317
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4036297
50 A = 6800863
08 meter
Y = -5397388
13 meter E =
0010625
Z = -952501
34 I = 51
96413
XDOT = 3312
977333 Wp = 46
71928
YDOT = 3517
835825 meter/sec RA = 120
44247 deg
ZDOT = -5929
528898 TA = 143
51473
MA = 143
44229
Ha = 231
646 n
mi
Hp = 218
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13242445
87 X = 4100979
17
Y = -17707966
29 feet Y = -5351890
10 meter
Z = -3125004
40 Z = -932736
32
XDOT = 10869
348207 XDOT = 3302
197706
YDOT = 11541
456119 feet/sec YDOT = 3554
823181 meter/sec
ZDOT = -19453
834967 ZDOT = -5913
461179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16669972
09 X = -5081007
49
Y = 14544878
73 feet Y = 4433279
04 meter
Z = -3042799
47 Z = -927445
28
XDOT = -7272
486144 XDOT = -2216
653777
YDOT = -12366
597731 feet/sec YDOT = -3769
338988 meter/sec
ZDOT = -19387
699744 ZDOT = -5909
370882
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12241
56269606
00016717 00000-0 10270-3 0 9120
2 25544 51
6453 121
2275 0015091 5
6372 354
4946 15
50040533 29276
Satellite: ISS
Catalog Number: 25544
Epoch time: 12241
56269606 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 121
2275 deg
Eccentricity:
0015091
Arg of perigee: 5
6372 deg
Mean anomaly: 354
4946 deg
Mean motion: 15
50040533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2927
Checksum: 290
Coasting Arc #14 (Orbit 2942)
---------------------------------------
Vector Time (GMT): 2012/242/12:46:23
265
Vector Time (MET): N/A
Weight (LBS) : 954317
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3747206
36 A = 6800399
22 meter
Y = 5504734
27 meter E =
0026267
Z = 1293040
25 I = 51
97710
XDOT = -3336
521761 Wp = 32
76099
YDOT = -3656
942808 meter/sec RA = 115
51095 deg
ZDOT = 5865
242713 TA = 341
24190
MA = 341
33851
Ha = 231
758 n
mi
Hp = 218
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12293984
12 X = -3814764
11
Y = 18060151
81 feet Y = 5462453
00 meter
Z = 4242258
03 Z = 1274672
48
XDOT = -10946
593703 XDOT = -3323
872568
YDOT = -11997
843857 feet/sec YDOT = -3694
182863 meter/sec
ZDOT = 19242
922286 ZDOT = 5849
065255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15560956
99 X = 4742979
69
Y = -15356122
40 feet Y = -4680546
11 meter
Z = 4165813
77 Z = 1269740
04
XDOT = 7432
557470 XDOT = 2265
443517
YDOT = 12764
613519 feet/sec YDOT = 3890
654201 meter/sec
ZDOT = 19176
342067 ZDOT = 5844
949062
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12242
59422077
00016717 00000-0 10270-3 0 9138
2 25544 51
6448 116
1158 0015252 9
1603 350
9823 15
50099101 29436
Satellite: ISS
Catalog Number: 25544
Epoch time: 12242
59422077 = yrday
fracday
Element set: 913
Inclination: 51
6448 deg
RA of node: 116
1158 deg
Eccentricity:
0015252
Arg of perigee: 9
1603 deg
Mean anomaly: 350
9823 deg
Mean motion: 15
50099101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2943
Checksum: 288
Coasting Arc #15 (Orbit 2957)
---------------------------------------
Vector Time (GMT): 2012/243/12:46:23
265
Vector Time (MET): N/A
Weight (LBS) : 954317
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3495978
13 A = 6799980
71 meter
Y = -5597199
56 meter E =
0011842
Z = -1669859
20 I = 51
98697
XDOT = 3355
080718 Wp = 43
24229
YDOT = 3799
497879 meter/sec RA = 110
58111 deg
ZDOT = -5727
094003 TA = 154
89844
MA = 154
84083
Ha = 231
839 n
mi
Hp = 217
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11469744
51 X = 3566419
00
Y = -18363515
63 feet Y = -5557711
62 meter
Z = -5478540
68 Z = -1652704
71
XDOT = 11007
482672 XDOT = 3340
165032
YDOT = 12465
544222 feet/sec YDOT = 3836
932685 meter/sec
ZDOT = -18789
678489 ZDOT = -5710
831954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14543677
20 X = -4432912
81
Y = 16063402
00 feet Y = 4896124
93 meter
Z = -5407099
32 Z = -1648083
87
XDOT = -7594
040276 XDOT = -2314
663476
YDOT = -13160
305320 feet/sec YDOT = -4011
261062 meter/sec
ZDOT = -18722
759481 ZDOT = -5706
697090
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12243
56126908
00016717 00000-0 10270-3 0 9141
2 25544 51
6441 111
3243 0015176 12
5596 347
5930 15
50075622 29584
Satellite: ISS
Catalog Number: 25544
Epoch time: 12243
56126908 = yrday
fracday
Element set: 914
Inclination: 51
6441 deg
RA of node: 111
3243 deg
Eccentricity:
0015176
Arg of perigee: 12
5596 deg
Mean anomaly: 347
5930 deg
Mean motion: 15
50075622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2958
Checksum: 299
Coasting Arc #16 (Orbit 2973)
---------------------------------------
Vector Time (GMT): 2012/244/12:46:23
265
Vector Time (MET): N/A
Weight (LBS) : 954317
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3203738
24 A = 6799329
52 meter
Y = 5632456
42 meter E =
0026171
Z = 2003389
02 I = 51
99417
XDOT = -3439
853385 Wp = 40
84523
YDOT = -3958
007321 meter/sec RA = 105
65007 deg
ZDOT = 5605
027636 TA = 341
17095
MA = 341
26756
Ha = 231
926 n
mi
Hp = 217
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10510952
23 X = -3276215
30
Y = 18479187
73 feet Y = 5596225
15 meter
Z = 6572798
63 Z = 1987649
10
XDOT = -11285
608218 XDOT = -3422
566042
YDOT = -12985
588322 feet/sec YDOT = -3996
376763 meter/sec
ZDOT = 18389
198280 ZDOT = 5588
359555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13343464
99 X = 4067088
13
Y = -16576202
54 feet Y = -5052426
54 meter
Z = 6507198
25 Z = 1983394
03
XDOT = 7989
827870 XDOT = 2435
299535
YDOT = 13652
101484 feet/sec YDOT = 4161
160532 meter/sec
ZDOT = 18320
614795 ZDOT = 5584
123389
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12244
59277634
00016717 00000-0 10270-3 0 9159
2 25544 51
6433 106
2119 0015225 16
1131 344
0501 15
50128282 29745
Satellite: ISS
Catalog Number: 25544
Epoch time: 12244
59277634 = yrday
fracday
Element set: 915
Inclination: 51
6433 deg
RA of node: 106
2119 deg
Eccentricity:
0015225
Arg of perigee: 16
1131 deg
Mean anomaly: 344
0501 deg
Mean motion: 15
50128282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2974
Checksum: 278
Coasting Arc #17 (Orbit 2988)
---------------------------------------
Vector Time (GMT): 2012/245/12:46:23
265
Vector Time (MET): N/A
Weight (LBS) : 954317
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2956214
99 A = 6798680
36 meter
Y = -5655471
07 meter E =
0013860
Z = -2371097
20 I = 51
99812
XDOT = 3521
961613 Wp = 41
61862
YDOT = 4104
103913 meter/sec RA = 100
72020 deg
ZDOT = -5405
993317 TA = 164
61304
MA = 164
57086
Ha = 232
006 n
mi
Hp = 217
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9698868
07 X = 3030754
06
Y = -18554695
12 feet Y = -5621996
29 meter
Z = -7779190
30 Z = -2356554
59
XDOT = 11554
992170 XDOT = 3502
067745
YDOT = 13464
907850 feet/sec YDOT = 4143
376926 meter/sec
ZDOT = -17736
198546 ZDOT = -5388
932681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12270425
41 X = -3740025
67
Y = 16991805
80 feet Y = 5179102
41 meter
Z = -7718532
92 Z = -2352608
83
XDOT = -8404
717163 XDOT = -2561
757791
YDOT = -14082
009321 feet/sec YDOT = -4292
196441 meter/sec
ZDOT = -17666
007578 ZDOT = -5384
599110
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12245
55980800
00016717 00000-0 10270-3 0 9163
2 25544 51
6423 101
4199 0015258 19
6736 340
5000 15
50115986 29892
Satellite: ISS
Catalog Number: 25544
Epoch time: 12245
55980800 = yrday
fracday
Element set: 916
Inclination: 51
6423 deg
RA of node: 101
4199 deg
Eccentricity:
0015258
Arg of perigee: 19
6736 deg
Mean anomaly: 340
5000 deg
Mean motion: 15
50115986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2989
Checksum: 309
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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